PAULL (Propulsion for uAlberta Undergraduate Liquid Launches)

The PAULL-01 liquid rocket is a project designed and conducted by the Student Team for Alberta Rocketry Research at the University of Alberta. Our team is developing a 5 kN liquid rocket engine that uses ethanol and nitrous oxide propellants. The design incorporates modern features such as regenerative and film cooling for reusability, along with a like-unlike injector to ensure efficient and stable combustion.

To ensure safety and reliability, PAULL-01 is undergoing.